View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52645U 26145.09869961 +.00000000 +00000-0 -51814-4 0 00005
2 52645 53.2125 276.2139 0001399 84.7983 275.3169 15.08842507 06
| Epoch (UTC): | 25 May 2026 02:22:07 |
| Eccentricity: | 0.0001399 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 276.2139° |
| argument of perigee: | 84.7983° |
| revolutions per day: | 15.08842507 |
| mean anomaly at epoch: | 275.3169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|